Diamond DA20 — Weight And Balance
1 weight and balance reference for the Diamond DA20.
Overview
DA-20 AIRPLANE PPL(A)
This document serves as a weight and balance reference for the Diamond DA20 aircraft, providing essential data for pilots and aviation enthusiasts. It includes specifications on the aircraft's dimensions, engine details, fuel system, and weight limitations. The manual is designed to ensure safe operation by detailing maximum weights, center of gravity limits, and performance parameters. It is crucial for pilots to understand these limitations to maintain safety and compliance during flight operations.
- Maximum takeoff weight: 750 kg (for OM-KLS)
- Maximum baggage weight: 20 kg
- Fuel capacity: 76 liters (usable: 74 liters, unusable: 2 liters)
- Engine: Rotax 912, 80 HP, max RPM 2550
- Stall speeds: 39 KT (T/O flaps), 41 KT (flaps up), 37 KT (landing flaps)
1 document